Douglas DC-8-73F
Service difficulty reports · 15,471
Newest first. General aviation reporting is voluntary.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE aircraft_model_key = 'DC873F' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE aircraft_model_key = 'DC873F' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR DHLA201100031Skin · misrepairedR & R EXISTING REPAIR AT FS 1531.000 - 1544.000 L21L UTILIZING APPROVED DATA (REF REPAIR REPORT F088) PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 02-18-11, EVA D853-00393 REV IR DATED 02-03-11, SMN DWG ED-5309 DATED 01-21-11, JC EC-02376-001 WO 9960. REMOSDR DHLA201100030Skin · damagedRUDDER RT SKIN BROKEN STA ZR 217.188. PERFORMED MAJOR REPAIR IAW SRM 55-6-1, FIG 1. REMOVED DAMAGED PANEL PLATING IAW SRM 55-1-0 PG 1, SRM 51-1-21. FABRICATED PLATING + BONDED FINGER DOUBLER BOTH FROM AL2024T3 0.016 " IAW SRM 55-6-1 FIG 1, ITEM "A". BONDED BOSDR DHLA201100022Rib · damagedRT RUDDER RIB BROKEN AT STA ZR 217.188 AFT OF SPAR PERFORMED MAJOR REPAIR IAW JC EC-02401-001 WO 9960, DWG 5654863, MS NR SEU-SEU-11-0007-02B DATED 01-25-11. REMOVED DAMAGED RIB IAW SRM 51-1-21, SRM 51-1-20D. FABRICATED RIB IAW DWG 5654863, HEAT TREATED IAW SRSDR DHLA201100033Plate · misrepairedINSPECT EXISTING REPAIR AT FS 670.000 - 684.000 L29R -L29L FOR CONDITION, SECURITY AND CONFORMITY WITH THE SRM. IF CONFORMS, PLEASE NOTE THE DETAILS ON THE NON ROUTINE AND ANY RE-INSPECT REQUIREMENTS (REF REPAIR REPORT F066) PERFORMED MAJOR REPAIR IAW FAA FORMSDR DHLA201100016Skin · misrepairedREMOVED DAMAGED PANEL PLATING IAW SRM 55-1-0 PG 1, SRM 51-1-21. FABRICATED NEW PLATING & BONDED FINGER DOUBLER IAW SRM 55-6-1 FIG. 1 ITEM "A". BONDED BOTH PARTS WITH HYSOL IAW SRM 51-1-9 TR 51-142, SRM 51-1-9A, TR 51-141, DPS 1.950 REV "AR" R-1. CLEANED, TREATSDR DHLA201100007Skin · misrepairedREMOVED NON STANDARD REPAIR & EXISTING SPLICES IAW SRM 51-1-21, SRM 51-1-20D. FABRICATED REPAIR DOUBLER & 2EA SPLICES IAW SRM 53-2-5 FIG. 15 SHEET 1-2, SRM 53-2-5 FIG. 15 SHEET 3, 4, 5 TR 53-179, SRM 53-4-1 FIG. 17A ITEM "A". HEAT TREATED REPAIR DOUBLER & SPLISDR DHLA201100006Skin · misrepairedREMOVED EXISTING NON STANDARD REPAIR IAW SRM 51-1-20D. FABRICATED REPAIR DOUBLER IAW SRM 53-2-0 FIG. 22A SHEET 2, 5, 12, 13, 14 TR 53-170, SRM 53-4-1 FIG. 11 ITEM "L". NDT INSPECTED REPAIR DOUBLER IAW NDT SPM PART 8, SRM 53-2-0 FIG. 22 SHEET 12 ITEM 23 TR 53-1SDR DHLA201100005Skin · misrepairedREMOVED EXISTING NON STANDARD REPAIR IAW SRM 51-1-20D. FABRICATED REPAIR DOUBLER IAW SRM 53-2-0 FIG. 22A SHEET 2, 3, 12, 13, 14 TR 53-170, SRM 53-4-1 FIG. 9 ITEM "A". NDT INSPECTED REPAIR DOUBLER IAW NDT SPM PART 8, SRM 53-2-0 FIG. 22 SHEET 12 ITEM 23 TR 53-SDR DHLA201100004Skin · misrepairedINSPECT EXISTING REPAIR ON RT FUSELAGE AT FS 230.000- 240.000, L21R FOR CONDITION & SECURITY. PERFORMED MAJOR REPAIR IAW SRM 53-2-5 FIG. 15 SHEET 1-2, SRM 53-2-5 FIG. 15 SHEET 3-5, TR 53-179 DATED 09-20-03. REMOVED EXISTING NON STANDARD REPAIR DOUBLER & SPLISDR DHLA201100028Skin · damagedRT WING UPPER PANEL DELAMINATED AND HOLES ELONGATED (STA XW 0.000 - 47.000) R & R RT WING UPPER PANEL (STA XW 0.000 - 47.000) IAW SRM 51-3-0, SRM 51-3-1 (TORQUE).SDR DHLA201100024Panel · delaminatedLT WING UPPER PANEL DELAMINATED STA XA 566.000 - 586.000. R & R LT WING UPPER PANEL WITH SAME FASTENERS IAW SRM 51-3-0, SRM 51-3-1 (TORQUE).SDR IXXA110004OPin · shearedDURING CLIMB OUT, AFTER GEAR RETRACTION, CREW NOTICED AN UNSAFE GEAR LIGHT INDICATION. ACCOMPLISHED UPLATCH CHECK, AND WHEN CYCLING THE GEARS FELT A VIOLENT SHUDDER AND THE LT MLG DOWN LIGHT ILLUMINATED INTERMITTENTLY. RETURNED TO DEPARTURE AND LANDED WITHOSDR DHLA201100038Frame · wornNR 3 ENG RT T/R STRUCTURAL FWD FRAME HAS EXISTING WEAR DAMAGE AT STA, YN 202.000 BETWEEN 5 AND 6 O'CLOCK POS. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 02-14-2011, EVA D878-00387 REV IR DATED 01-28-11, SMN DWG ED-5312 DATED 01-24-11. REMOVED FASTENERS SDR DHLA201100018Frame · wornNR 4 ENG RT THRUST REVERSER STRUCTURAL FWD FRAME HAS WEAR DAMAGE AT STA YN 202.000 BETWEEN 5 AND 6 O'CLOCK POS PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 02-11-11, EVA D878-00389 REV IR DATED 01-31-11, SMN DWG ED-5311 DATED 01-25-11. REMOVED FASTENERS IASDR DHLA201100017Frame · wornNR 4 ENG LT THRUST REVERSER STRUCTURAL FWD FRAME HAS WEAR DAMAGE STA YN 202.000 BETWEEN 7 AND 9 O'CLOCK POS PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 02-15-11 EVAD878-00388 REV IR DATED 01-28-11, SMN DWG ED-5310 DATED 01-24-00. REMOVED FASTENERS IAW SRMSDR IXXA110002OMechanism · out of adjustDURING CLIMB OUT, THE DOOR NOT LATCH LIGHT CAME ON WITH GEAR RETRACTED. THE CREW CYCLED AND ACCOMPLISHED UPLATCH CHECK AND DOOR NOT LATCH LIGHT REMAINED ON. THEY RETURNED WITHOUT FURTHER INCIDENT. MX INSPECTED AND FOUND LT MAIN LANDING GEAR FOLLOW UP MECHANISDR IXXA110001OWarning Switch · arcedDURING CLIMB OUT, THE "DOOR NOT LATCH" LIGHT CAME ON WITH LANDING GEAR RETRACTED. THE CREW CYCLED GEAR AND ACCOMPLISHED UPLATCH CHECK, DOOR NOT LATCH LIGHT REMAINED ON THE REMAINDER OF FLIGHT. LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED AND FOUND FLUID COSDR DHLA201100001Battery Pack · inoperativeEMERGENCY EXIT LIGHTS ARE VERY DIM. ACFT WAS GROUNDED. R & R EMER EXIT LIGHTS POWER SUPPLY, OPS CHECK GOOD IAW AMM 33-50-1. EMERGENCY LIGHT CB WILL NOT RESET. R & R EMERGENCY LIGHT BATTERY PACK. SYS OPS CHECK GOOD IAW 33-50-00.SDR 2011F00016Power Supply · dischargedUPON CHECKING THE EMERGENCY LIGHTS FOUND THE LIGHTS TO BE VERY DIM. THE LIGHT POWER SUPPLY WAS REPLACED. OPS CHECKED SERVICABLESDR 2011F00015Power Supply · dischargedUPON CHECKING THE EMERGENCY LIGHTS FOUND THE LIGHTS TO BE VERY DIM. THE LIGHT POWER SUPPLY WAS REPLACED. OPS CHECKED SERVICABLE.SDR IXXA100060OConnector · looseDURING CRUISE NR 1 ENGINE FIRE WARNING AND BELL FLICKERED MOMENTARILY AT 410, SAT -50, TAT -21, MANIFOLD PRESSURE 32, MANIFOLD AIR TEP 150. THE CREW TESTED FIRE WARNING AND SHORT CIRCUIT WERE NORMAL CONDITION, REMAINED NORMAL REST OF FLIGHT. THEY LANDED IN KSJSDR IXXA100058SSkin · crackedDURING WALK AROUND, FOUND A CRACK ON BELLY CTR LINE LONGERON 36 AT STA 1400. MX REPAIRED IAW SRM 53-2-1 CLASS 3. ACFT WAS RETURNED TO SERVICE.SDR U2RA485FLP5226Inu · inoperativeNR1, IMMEDIATELY AFTER ROTATION, NR 1 INU FAILED, CAPT INSTRUMENTS FLAGGED FAIL. NR 2, IMMEDIATELY AFTER ROTATION GPWS WENT INOP. NR 3, IMMEDIATELY AFTER ROTATION YAW DAMPER KICKED OFF AND A/P OR YAW DAMPER WOULD NOT ENGAGE FROM EITHER PILOTS A/P TRANSFER SWSDR DHLA201000152Access Door · corrodedACCESS DOOR HAS CORROSION AT FUSELAGE STA FS 650.000 L32R - L36. PERFORMED MAJOR REPAIR IAW ASTAR EC-02354-001 AND DWG 5800471 AND WO 9735. REMOVED CORRODED ACCESS DOOR IAW DPS 3.67 AND SRM 51-3-0. REMOVED CORROSION IAW SRM 51-1-8. FOUND OUT OF LIMITS IAWSDR DHLA201000150Skin · damagedINSPECTED EXISTING REPAIR LOCATED AT FS 1890.000, L36 FOR CONDITION, SECURITY AND CONFORMITY. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3, DATED 12-09-10 AND EVA D853-00384 REV "IR" DATED 11-18-10. REMOVED EXISTING REPAIR IAW SRM 51-1-21. TRIMMED OUT DAMAGED ASDR IXXA100057SSkin · puncturedPUNCTURE IN LT FWD SIDE OF FUSELAGE AFT AND ABOVE OF LT ACM HEAT EXCHANGE LOUVER DOORS. REPAIRED IAW 53-10653-1. ACFT RETURNED TO SERVICE.SDR DHLA201000151Spar Cap · crackedNR 1 ALT TANK FRONT SPAR LWR CAP SPLICE CRACKED 1" STA XFS 532.000 S-64 PERFORMED MAJOR REPAIR IAW EC-02340-001, WO 9735, MESSAGE SEU-SEU-10-0074-028, DATED 11-17-10. REMOVED CRACKED SPLICE FITTING IAW JC EC-02340-001, MESSAGE SEU-10-0074-028 AND DWG 3644046.SDR DHLA201000142Skin · corrodedFUSELAGE SKIN BULGING AND CRACKED BETWEEN 2 FASTENERS AT FS 1447.0, BETWEEN LONGERONS 30R AND 29R. ACCOMPLISHED FUSELAGE SKIN DOUBLER AND FILLER REPAIR IAW EVA D853-00386 REV IR, DWG NR D85300386-001-D, REV IR, AND SRM CHAPTERS 51 & 53. HFEC OF REPAIR PARTS SDR DHLA201000139Wire · brokenCLIMBING OUT OF 2000 FT AFE ENG NR 4 FIRE INDICATION. COMPLETED PHASE I'S AND ENG FIRE CHECKLIST FIRED BOTH BOTTLES. EMERGENCY WAS DECLARED. AIR TURN, ACFT WAS GROUNDED. INSPECTED NR4 ENGINE AND FOUND NO EVIDENCE OF FIRE IAW MM71-00-00. R & R NR3 AND NR4 FIRSDR DHLA201000140Skin · bulgedFUSELAGE SKIN BULGING AND CRACKED BETWEEN 2 FASTENERS AT FS 1447.0, BETWEEN LONGERONS 30R AND 29R. ACFT WAS GROUNDED COMPLIED WITH EVA D853-00386 DWG D85300386-001-D AND NR 9855-2.SDR DHLA201000138Engine · power lossENG NR1 ROLLED BACK ON CLIMBOUT. PERFORMED ENG SHUTDOWN & RE-LIGHT. NO FUTHER PROBLEMS. ACFT WAS GROUNDED UPON ARRIVAL. C/W TROUBLESHOOTING IAW MM AND MM 71-00. NO FAULTS NOTED. RAN ENG IAW JRH 12.6. OPS CHECKS SERVICEABLE.SDR DHLA201000137Control Valve · shearedLT BRAKE INOP, BRAKE PRESSURE NORMAL. ACFT WAS GROUNDED. REPLACED WHEEL BRAKE CONTROL VALVE ASSY IAW MM 32-42-2. SYS OPS NORMAL, OK FOR SERVICE.SDR IXXA10SMN114SSkin · damagedDURING ROUTINE C-CHECK INSP FOUND LT WING T/E LOWER SKIN HAS IMPROPER REPAIR AT STA XW 730.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN AND FINGER DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATSDR IXXA10SMN113SFitting · crackedDURING ROUTINE C-CHECK INSP, FOUND MAIN CARGO COMPARTMENT FWD FITTING CRACKED AT STA 902.000 LONG 19 LT. REMOVED CRACKED FITTING. CLEANED, TREATED, AND PRIMED AREA. SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-1-8B, SRM 51-1-20D, SRM 51-3-1.SDR IXXA10SMN112SWeb · crackedDURING ROUTINE C-CHECK INSP FOUND NR 3 MAIN TANK WEB CRACKED AT STATON XRS 168.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED STRAP, SHIMS, SPLICES, FILLER, ANGLE, TEE, AND FISDR IXXA10SMN111SSkin · damagedDURING ROUTINE C-CHECK INSP FOUND LT WING T/E UPPER SKIN DOUBLER WITH IMPROPER REPAIR AT STA XW 736.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND FINGER DOUBLERS. BONDED PARTS AS NEEDED WITH HYSOL. CLEANSDR IXXA10SMN110SSpar Cap · crackedDURING ROUTINE C-CHECK INSP, FOUND NR 3 MAIN TANK LOWER CTR SPAR CAP AND WEB CRACKED AT STA XRS 168.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED STRAP, SHIMS, SPLICES, FILLERSDR IXXA110039SFloor Panel · corrodedDURING ROUTINE C-CK INSP FOUND MAIN CARGO COMPARTMENT FLOOR PANEL SKIN CORRODED BETWEEN STA 1060.000 LT BOTTOM LINE10. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED DOUBLERS AND FILSDR IXXA10SMN109SLongeron · corrodedDURING ROUTINE C-CHECK INSP FOUND MAIN CARGO COMPARTMENT AFT SECTION FLOOR LONGERON 36 CORRODED AT STA 1690.000 - 1725.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED LONGERON SEGMENT. FABRICATED LONGERON AND STRAPS. CLEANED, TREATED, PRIMED ARESDR IXXA10SMN108SFitting · crackedDURING ROUTINE C-CHECK INSP, FOUND MAIN CARGO COMPARTMENT AFT FITTING CRACKED AT STA 781.000, LONGERON 19 & 20 RT. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED CRACKED FITTING. CLEANED, TREATED, AND PRIMED AERA. INSTALLED NEW FITTING IAW SRM 51-1-8, SRSDR IXXA10SMN107SFitting · crackedDURING ROUTINE C-CHECK INSP, FOUND MAIN CARGO COMPARTMENT AFT FITTING CRACKED AT STA 857.000, LONGERON 19 & 20 RT. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED CRACKED FITTING. CLEANED, TREATED, AND PRIMED AERA. INSTALLED NEW FITTING IAW SRM 51-1-8, SRSDR IXXA10SMN106SFitting · crackedDURING ROUTINE C-CHECK INSP, FOUND MAIN CARGO COMPARTMENT AFT FITTING CRACKED AT STA 1160.000, LONGERON 20RT. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED CRACKED FITTING. CLEANED, TREATED, AND PRIMED AERA. INSTALLED NEW FITTING IAW SRM 51-1-8, SRM 53SDR IXXA10SMN105SFitting · crackedDURING ROUTINE C CHECK INSP FOUND MAIN CARGO COMPARTMENT FITTING CRACKED AT STA 717.000 LT BOTTOM LINE 22. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED CRACKED FITTING. CLEANED, TREATED, AND PRIMED AERA. INSTALLED NEW FITTING IAW SRM 51-1-8, SRM 53-2-0SDR IXXA10SMN104SFitting · crackedDURING ROUTINE C-CHECK INSP, FOUND MAIN CARGO COMPARTMENT FITTING CRACKED AT STA 700.000, LT BOTTOM LINE 23. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED CORRODED FITTING. CLEANED, TREATED, AND PRIMED AERA. INSTALLED NEW FITTING IAW SRM 51-1-8, SRM 53-SDR IXXA10SMN103SFitting · corrodedDURING ROUTINE C-CHECK INSP FOUND MAIN CARGO COMPARTMENT FITTING CORRODED AT STATION 960.000 - 980.000 RT BOTTOM LINE 28. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED CORRODED FITTING. CLEANED, TREATED, AND PRIMED AERA. INSTALLED NEW FITTING IAW SRM 51SDR IXXA10SMN102SSkin · delaminatedDURING ROUTINE C-CHECK INSP FOUND RT ELEVATOR T/E LOWER SKIN CRACKED AND DELAMINATED AT STA XE 77.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATEDSDR IXXA10SMN101SSkin · crackedDURING ROUTINE C-CHECK INSP FOUND RT ELEVATOR T/E LOWER SKIN CRACKED AND DELAMINATED AT STA XE 132.750. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATESDR IXXA10SMN115SSkin · corrodedDURING ROUTINE C-CHECK INSP FOUND LT WING L/E LOWER PART CORRODED ST STATION XFS 335.250 - 341.500. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO CRACK OR CORROSION NOTED. FABRICATED DOUBLER AND FILLERS. CLEANED, TREASDR IXXA10SMN100SSkin · brokenDURING ROUTINE C-CHECK INSP, FOUND LT INBD FLAP UPPER SKIN BROKEN AT STA XW 107.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIRSDR IXXA10SMN099SSkin · corrodedDURING ROUTINE C-CHECK INSP, FOUND LT OTBD FLAP LOWER SKIN CORRODED AT STA XF 407.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND DOUBLER. BONDED PARTS AS NEEDED WITH
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